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Elastic properties and fracture strength of quasi-isotropic graphite/epoxy composites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sullivan, T. L. |
| Copyright Year | 1977 |
| Description | The layups of the studied laminates are (0, + or - 60) sub s, (0, + or - 45, 90) sub s, (0, + or - 30, + or - 60, 90) sub s (0, + or - 22 1/2, + or - 45, + or - 67 1/2, 90) sub s. The properties determined were tensile modulus, Poisson's ratio, bending stiffness, fracture strength and fracture strain. Measured properties and properties predicted using laminate theory were found to be in reasonable agreement. Reasons for data scatter were determined. |
| File Size | 1590083 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770010221 |
| Archival Resource Key | ark:/13960/t58d4q17t |
| Language | English |
| Publisher Date | 1977-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Fiber Strength Poisson Ratio Tensile Deformation Carbon Fiber Reinforced Plastics Elastic Properties Fracture Strength Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
